ML20082G667

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NMSS Equipment Qualification Summary for Main Steam Relief Valves
ML20082G667
Person / Time
Site: LaSalle  Constellation icon.png
Issue date: 05/29/1981
From:
SARGENT & LUNDY, INC.
To:
Shared Package
ML20082G653 List:
References
NUDOCS 8311300291
Download: ML20082G667 (24)


Text

.

7/

LA SALLE NUCLEAR STATIONS' j

O uN11 182 NSSS EQUIPMENT QUALIFICATION

SUMMARY

EQUIPMEt4T NAME :

Main Steam Safety Relief Valves i

EQUIPMENT NO:

1.2B21-F033A/H, J/N,P,R,S,U & V I

LOCATION:

Primary Containment EQUIPMENT CLASSIFICATION:

@ ACTIVE

] PASSIVE Test i

OUALIFICATION METHOD:

f

14. Wyle Lab Test Report #44640-1, dated 8/20/79.
15. Dwg. #DS-A-63825, Sheet 1.

i OUALIFICATION DOCUMENT

REFERENCES:

Inte'roffice Memo and Form MAS EMD-2.4.

1.

I 2.

Summary of accelerations and nozzle loads.

,k 3.

Test Report, Wyle Lab. Report #43415-2, dated 8/20/79.

Interoffice Memo of acceptability of S&L piping analysis.

4.

SRV Accelerations Table, GE piping analysis EMD # 030499 g

3.

6.

Project sheet GEVPF #921D886F, Sh. No. 1,2 & 3.

l Specification GE22A6441, dated 4/11/79.

7.

I Drawings, Crosby Dwg. #DS-A-63790, sht.

1,2,

& 3, dated 8/2/79 g,

(GE VPF # 6115-(l)-2) 9.

Data Sheet, GE Doc. #386HA603, dated 3/24/77.

!E 10./13. Analysis Report & Addendums, Crosby Co. Report No. 3012 for EMD No. 002533 (GE VPF #3097-67-2)

LOAD COMBINATIONS CONSIDERED IN QUALIFICATION:

y g

1.

Normal Operating Loads + OBE +

SRVASY-TQ +

ALL-TO, ENVELOP

'?d 2.

Normal Operating Loads + SSE + COLEVY-2+ SRVASY-TO+

ALL-TO, ENVELOP:

'y j I

RV337_79 + SRVALL-TO ENVELOP!

er Norma 1 Operating Loads + SSE+ Chugging +

3.

l' 4.

Normal Operating Loads + SSE + AP 5.

Normal Operating Loads + SSE + COLEVY-1 r

I

[

f.UALI F IC AT ION :

E'2 b8!

8, r/f7af/274L Date PRi:PAnl:D BY:

/d Date f-2f-8/

SARGE.1T& LUNDY \\

REVU;;;!:D BY:

M :?D W:

jf Date q.jej. fI T}

B311300291 831128 PDR ADOCK 05000373 P

PDR

.em__...,.,-

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P s

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QUALIFICATION

SUMMARY

l.

seismic Qualificatio'n Method:

l.

Resonance Search Conducted in each of the three principal axes with a low level (approximately 0.2g) sine sweep from 1 to 40 Hz at a sweep rate of one octave per minute.

2.

Specimen subjected to 30 second duration biaxial phase incoherent 3 random input consisting of frequency band widths spaced one-thirds octare apart over the frequency range-1 to 40 Hz.

3.

The amplitude of input was independently adjusted in each direction until TRS enveloped the given RRS.

4.

During the entire testing, inlet and outlet flanges were subjected to 400000 and 300000 inch-pound moments respectively.

5.

Five OBE tests and one SSE test performed in each biaxial plane.

l 6.

Extended load tests were conducted similar to above tests with the following modification.

a)

Inlet and outlet flanges were subjected to 800000 and

'i 600000 inch-pound moments respectively.

l i

b)

SSE test durations are 15 sec. each.

7.

Valve was tested for operability during the entire ceismic testing.

o SRV Requalification Method:

Loads resulting from the analysis of the piping using the hydro-j dynamic laod combinations will be limited to the laods to which l

g the valves are qualified.

]

t I

A**

O i

o w

i t

.I

+

N s

4 j

Ref: EMD File No. fftD-o3e8o3

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"""""c=hrsk--mma 2 _ _wr. _. _., _. m m;Q,,j

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.. +.

.w m,nn n.-

- m.

.),;g,

. 4 --r g

J.,

Oualification Summr/ of Equirrent I'aSalle County - l& 2 g;

T.

Plant ?bre:

1.

Utility: Commonwea1th Edison Co.

M M

X

' 2.

NSSS:

General Electric 3.

A-E:

Sargent & Lundy biain Steam Safety Relief Valves ll II.

Conponent Nre

,c l

1.

bbdel Nu:rber 6xRx10 HP-Bp Quantity:

23 Gace Co.

l 2.

Vendor General Electric co_ /N+j mn.g e

3.

If the ccuponent is a cahmet or panel, nann and hodel Ib. of l

the devices incitxied.

4.

Physical Description a.

Appearance Relief Valve I

i l

b.

Dinensions Inlet -

5",

outl et 10" f

l N.

i c.

Weight 2800 lbs.

5.

Iocation: Building:

Primarv Containment s

Elevation; On Main Steam Piping syetem 6.

Field bbunting Conditions [

]

Bolt (tb.

, Size

)

[ ]

Weld (Length

)

j' Pine Fountad (X]

l 7.

Natural Frequencies in Each Direction:

O bl:

20, 22.5 h2:

22.5 V: none below 40 Hz

g F

I 8.

a.

Functional D2scription: Provide automatic depressuri-:

~

zation of the reactor vessel and relief pressute 9

7 discharce to the suceression cool via a closedf discharce piping path ji h

Is the equiprent required fori }Ibt Standby [ ] Cold b.

3 Shutdan

[X]Doth

,e (e

M 9.

Pertinent Ibference Design Specifications:

J I

G.E.

Spec. 222A6441 1

ii Fcference: 120 File th.E Mry- 030883 8ANbEIN I EUIl0Y 1

'~

_._: ~ w a a u n,-

~

^

E&g

_ 7NN P O IM N#

3 U * *O 4TN Y WA. m&&;m.a.

.-.mm nc -

v

--c emg w

j If Qualification by Analysis or by the Corbimtion of Test ard Amlysis,the VII.

Orplete:

N/A li Inscription of Test including Results:

2.

M2thod of Analysis:

[

] Static Analysis

[ ] Equivalent Static Analysis [ ] Dynamic

(

Analysis

[

} Response Spectrum [

] Tine-History 3.

Pbdel Type:

[ l 3D

[ ] 2D

[D ll h [ ] Finite Elem2nt[ JBeam [ ] Closed Form Solution ~ 4. [ ] Conputer Codes: Frequency Pange and No. of nodes considered: e [ ] Hand Calculations 5. Damping: i 6. Support Considerations in the model-7. Critical Structural Elenents: Governing Seismic Total Stress A. Identification Iccation Resconse Qxbination Stress Stress Allcuablei i l 1, o i N W EffectUponPunctionalj .1 N B. Mw. Deflection location Operability j k h t 0 1 4 f, 1 i 1 h l mference: an File te. 6Mp-03og,,3 SARGENT LUl;DY ' !i. _s_ - t N fJ IN E' ef 54 0 w,j NW(&N YY.~O CT.0 $ & f, hfg gt*%* TJ n3T4HD,*[l[% "W_ -~

1.,

mm

_gn,

(jb 111. Is Equittmnt Available for Insocction in the Plant [x] Yes [ ] Ib.. ~ l ComTents: 1 l IV. Equipent Qualification bbthed: Test: X i Analysis: I 02tbination of Test and Analysis: Test by: Wyle Iab.Pecort 543445-2. aatca 1/12/77 f (nane of Conpany or LaDoratory & Feport No.) b V. Vibration Input: Ioads considered 1.[ ] Seismic only 2.[ 1, Hydrodynamic only 3.[] Explosive

  • l.

only y 4.[ ] Other (Specify) 5.[X](bnoination of 1 & 2 i 3 2. Pequired Response Spectra (attach the graphs): [l-See attached Tables l d ( e 3. Required Acceleration in Each Direction: See attached Tables 6 I h hl = h2 = V= VI. If Qualification by Test, then Coculete: .] a 1 1. [ ] Single Frequency [X] Multi-Frequency 2. [ ] Single Axis [X] Multi-Axis L 3. Frequency Rame: 1 to 40 Hz } TRS enveloping RRS using Multi-Frequency Test [g Yes (Attach TRS grayi U 4. o ll ((. t See attached Tables { ] !b 5. g-level 'Ibst at h1 = h2 = V= i,' l-l J 6. Laboratory Sbunting: Specially designed modular fixture if 7 t to apply nozzle loading hi g i '? 1. I 1 Bolt (ib. Size ) [ ] Weld (Ieength )[ ] a i A* 7. Functional operability verified: [X] Yes [ ] tb [ ] Not Applicable y l N 8. Other tests perfonmd (such as fragility test, including results) ,j I. I f Resonance Search test. h i' SARGEiT o f.Ui:DY o! Peference: DD File tb. _FMB- 030ge3 - C r. O r A.2 Ec13 h 1 3 _.W'**T*yM W~N~-w~=yq=. _ _. ~ g--n e====,- = ="ry M r mV 7 mgSNMgq*ggWL,'y~* %f*;,;,_ v. no- _j{ ~ ~ = - -

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q_p _4 j j. I i 3 2 J 4 6 6 7 8 913 2 3 I 4 5 6 7 5 9 l0 2 3 4 5 6 - 1 10 100 J t' Frequency (Hz) ~ Axis M* !WM LOCATION NO. b TEST RUN NO. LID

SARGENT & LUNDY CNGlNCCRC = CHlCAGO ..w. c. Summary: Accelerations (g) Allowables (OBE/SSE) Actual (Faulted) from Ref. (A) Ref. (B) Ref. (C) Horizontal' OBE/SSE Pipe Lines (Longitudinal) 4.8/5.2 Line A Line B Line C Line D (Lateral) 4.5/5.2 or (Resultant) 3 6.6/7.3 2.8 . 2.9 2.6 2.7 Vertical 2 3.2/4.4 2.5 2.2 1.6 3.2 \\

References:

(A) Qualification Report (GE VPF #3097-67-2,i.e., Ref. #10) (B) Test Report (Wyle Lab. Report #43445-2,i.e., Ref. #7) (C) Diping Analysis (GE Report, Table 16, See page 2/5) i .l I i l A

SARGENT Q LUNDY EN GIN EE R S CHICAG3 i Equipment No. ' Inlet Pipeline Outlet Pipeline Reducing Plance B21-F013N 1MSO4AN8 1MS04BN12 C307LS (Yes) B21-F013L 1MSO4AL8 IMS04BL12 \\ ^ B21-F013R IMSO4AR8 1MSO4BR12 B21-F013E IMSO4AE8 1MSO4BE12 B21-F013C 1MSO4AC8 1MSO4BCl2 .B21-F013U 1MSO4AU8 1MSO4BU12 B21-F013G 1MSO4AG8 1MSO4BG12 B21-F013H 1MSO4AII8 IMSO4 Bill 2 B21-F013A .lMS'04AA8 1MSO4BAl2, B21-F013V. 1MSO4AV8 1MSO4BV12 B21-F013P 1MSO4AP8 1MSO4BP12 B21-F013J IMSO4AJ8 1MSO4BJ12 B21-F013B 1MSO4AI58 1MS04BB12 B21-F013M lMSO4AM8 1MS04BM12 B21-F013S IMSO4AS8 1MSO4BS12 .B21-F013K' 1MSO4AK8 1MSO4BK12 B21-F013F IMSO4AF8 1MSO4AF12 ~ B21-F013D IMS01AD8 1MSO4BD12 9 e 4 0 5 A. e

~ CARGENT & LUNDY ENGINEERG CHICA2O \\ LOADS COMBINATIONS Nozzl'e Loads from Ref. # (A) pg. 5 and pg. 19 Allowable tbzzle Inlet Moment = 800,000 in-lbs h ds (From Test Report) Outlet Moment = 600,000 in-lbs Nozzle Loads from Ref. # (B) for SRV Inlet / Outlet Actual Ibzzle Inlet Moment = See Table (I) on pg. 8/9 Ioads (From GE piping analysis) c., Outlet Moment = See Table (II) on page 10/11 e 0 l = I l l w- ~. --- -w. --..w5,,,.._ __,

~l CARGENT & LUNOY ' " ? ' "Jf "

  • INLET Real Nozzle Loads from Ref. # -(C):

TABLE (I)

Valve,

, Service F F M M 3 B C A .B C R No. ' Level (lb) (lb) (16) (in-lb) (in-lb) (in-lb) (in-lb) B21-F13V Nodn=043 D 11067 13945 13922 277812 405225 305159 578,367 B21-F13P Nodn=053 D 13736 13540 15101 174034 361214 563180 691,328 B21-F013J Nod =063 D 11394 10284 10711 103643 317959 332636 471,685 B21-F013B Nods =073 D 13900 10462 13544 281070 317967 312969 527,307 B21-F013M Node =043 D 9424 15811 9808 184201 38,6511 286755 515,314 B21-F013S pode=048 D 13162 13184 10212 158435 265598 329223 451,699 _h21-F013K Node =053 D 10897 8641 7555 103559 194994 222736 313,621 B21-F013F Node =058 D 10857 13242 9098 165623 201923 266100 372,845 B21-F013D Node =063 D 11103 12546 12338 169473 290317 219112 401,267 B21-F013N Node =043 D 12012 15509 11849 181538 495736 433673 683,215 B21-F013L i Node =048 D 7364 11092 11883 168334 329556 267129 456,401 B21-F013R Node =053-D 10895 12240 11123 143726 277568 330085 454,596 B21-F013E . Node =058 D 11747 12295 10695 180198 267072 267556 418,790 j m21-F013C ! Node =063 D 9699 7901 10145 77076 314086 209235 385,188

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_.m CARGENT & LUl[OY ~ E N O f N E E f#3 CH ECA*lo Real Nozzle Loads from Ref. # (C) : TABLE (I) (Continued) . Valve Service F F 3 B C A b C k N3. Level (lb) (lb) (lb) (in-lb) (in-lb) (in-lb) (in-lb) B21-F013U Nods =043 D 11703 10768 9728 173654 222496 342012 443,433 B21-F013G Node =053 D 11468 10339 8597 150376' 270693 342281 461,567 B21-F013H' Nods =06,3 D 12776 9992 '8853 158646 229880 354938 451,657 B21-F013A l Nods =073 D -10959 11762 13098 167935 226223 404423 552,092 i i (D " ~ All M listed above are less than the allowable moment, R the inlet flange is qualified at Service Level C & D = l I i l. ~ l i g . t i ..--.-..r--

CARGENT O LUNDY EN GINI ERG OUTLET Real Nozzle Loads from Ref.

  1. . (C.) :

TABLE (II) i Valve Service F F g B C "A "C "R B No. Level (lb) (lb) '(lb ) (in-lb) (in-lb) (in-lb) (in-lb) B21-F013V Nods =300 D 3679 3562 4615 95903 377462 250763 463,203 B21-F013P Node =200 D 3972 7200 2298 183083 155122 461648 520,289 D21-F013J Node =400 D 6371 4915 905 38396 90406 346051 360,544 B21-F013B Nods =500 D 8684 5212 3778 49070 292444 380450 453794 B21-F013M Node =100 D 2492 4151 2549 244894 152665 192699 347,005 D21-F013K Node =200 D 2351 6662 2265 67746 92782 263714 287,651 B21-F013S "7de=300 D 3480 7397 4236 124282 100686 270709 314,431 B21-F013F Node =400 D 1454 6689 1255 41533 69991 179821 291,417 B21-F013D Node =500 D 922 4697 2777 93721 137450 224696 279,579 B21-F013N Node =100 D 2228 6769 4632 345836 154369 198407 427,548 B21-F013R Node =200 D 3416 9447 2784 114386 139553 234414 295,819 B21-F013L Node =300 D 1848 6707 2255 86380 120987 334202 365,774 B21-F013E i Node =400 D 3991 7125 2953 97192 151797 279692 332,741 B21-F013C Node =500 D 10970 4276 2204 41098 69844 201529 217,212 D21-F013U Node =100 D 3470 3351 2884 102656 140114 334233 376,672 n21-F013G >de=200 D 3134 3796 2292 89102 124125 386407 415,519 B21-F013H Node =300 D 3837 5474 1819 71128 150616 389931 424 017 B21-F013A { Node =400 D 3195 9192 1846 74435 156798 402662 43E,473i

i. .CARGENTQ LUNDY 'l '.J ENGINEERS i CHICAt@ l i i, t g Summary of Piping Lines: (From P&I Diagram of LaSalle Station) l Qualification'of Inlet / Outlet Flanges: ~ (I) Inlet (A)/ Outlet (B) Nozzle Load Allowables at Service i Level C & D l (A) Inlet Nozzle Load Allowables Inlet flange studs: Material = SA~193 Gr. B7 Size = l-3/8" - 8UN-3A Stress Area = 1.2319 in (Mark's Handbook, page 8-13) No. of Studs'= 12 Diameter of Bolting Circle = 12-1/2 (Forged flange 1500 lb.B16.5) 2 Total Stud Stress Area = 12 x 1.2319 = 14.7828 in Per NC-3658.3, for flange bolting material which has an Sm i value at 100*F, not less than 20.0 ksi may be analyzed rm %,7 as following: Mfd < (11,250A (w /16) D -Pfd)C(Sy/36) for Service Load b f C& D where S = Yield Stress of flange material at design y temperature (SA105 Gr B) (585'F, Sh.#13 Specification) = 26.6 @ 600*F per Appendix Table 1-2.1) C = Diameter of bolt circle = 12.5 in 2 Ab = Stress area = 14.7828 in f = Outside diameter of raise'd face.= 8.56in D i (See Ref. attached) Pfd= Pressure concurrent with Mfd = 1375 psi Therefore, M 1 11250 (14. 7828) - (w/16 ) (8.56)2 (1375) fd (12.5) (26.6/36)= 1,353,312 in-lbs. = Bending or Torsional Moment including ~ dynamic loads. 1 f.

~ ~ CARGENT0LUNDY E N o1N EE RO i CHICAG3 (B) Outlet Nozzle Loads Allowable: Outlet flange studs: Material = SA 193.Gr. B7 Size = l-8UNC-2A 2 Stress Area = 0.606 in No. of Studs = 16 Diameter of Bolting Circle = 15-1/4 in 2 Total Stud Stress. Area = 16 x 0.606 = 9.696 in Same procedure as the inlet flange analysis. M i ll,250Ab= (w/16) D P ( Y! } fd g fd Service Load C&D where S = 29.1 ksi (Appendix, Table I-2.1) @ 500*F. (Specification SH.NO 14) C = 15.25 in Ab = 9.696 in Df = 12.4 in (12 inch to 10 inch reducing flange) 0,, '~ Pfd= 625 psi (Specification Sht. No. 14) Therefore, M 5 11250 (9.696) (w/16) (12.4) (625) = fd (15.25) (29.1/36) = 1,112,036 in-lbs. To analyze the flange under Service Level A & B, the . procedure of NC-3658-3 can be applied: (II) Inlet (A)/ Outlet (B) Nozzle Load Allowab'les at Service Level A & B. (A) For inlet flange at. Service Level A & B M 6250 (26.6/36) (12.5) (14.7828) fd = 853,347 in-lbs = Allowable torsional or bending moment Compare the actual nozzle loads of Service Level D which are tabulated in Table (I) to the allowable given above for Service Level A & B. All acturial resultant mo'ments are less than above allowable. Therefore, the inlet flange meets the requirement per NC-3658. I

~ CARGENT Q LUNDY t 'ENGINEERG CHICATO ,t r (B) For outlet flange ~at Service Level A & B M 6250 (29.1/36) (15.25) (9.696) fd = 747,021 in-lbs All loads of Service Level D are less than the Service Level A & B allowable given above, the outlet flange is qualified.

== Conclusion:== The GE piping analysis nozzle loads are acceptable. e .#S'. ' 7,, O 4 0 e 4 i .i 1 i \\ 1 i i j .}}